*HEADING
 Transfer from Standard to Explicit: Test for CAX6M element 
 - Standard analysis
 - loading in tension
*NODE,NSET=ALL
 1,
 2, 2., 0.
 3, 2., 2.
 4, 0., 2.
 5, 1., 0.
 6, 2., 1.
 7, 1., 2.
 8, 0., 1.
 9, 1., 1.
*NSET,NSET=SIDE
 3,4,7
*ELEMENT, TYPE=CAX6M, ELSET=SHELL
 10, 1,2,4,5,9,8
 20, 2,3,4,6,7,9
*SOLID SECTION, ELSET=SHELL, MATERIAL=STEEL
0.2
*MATERIAL,NAME=STEEL
*ELASTIC
 200.E9, 0.3
*DENSITY
 1000., 
*BOUNDARY
 1, 1,2
 2, 2,2
 4, 1,1
 5, 2,2
 8, 1,1
*RESTART,WRITE
**
**
*ELSET,ELSET=QA_TEST_ALLELEMS
SHELL,
**
*NSET, NSET=QA_TEST_ALLNODES
ALL, SIDE
**
*STEP,NLGEOM,INC=50
*STATIC
 0.1, 1.
*CONTROLS, PARAMETERS=FIELD, FIELD=DISPLACEMENT
 5.e-4,,,,
*BOUNDARY, TYPE=VELOCITY
 2, 1, 1, 0.2
 3, 1, 1, 0.2
 6, 1, 1, 0.2
*PRINT,FREQ=1
*EL PRINT,FREQ=1
 S,
 E,
 PEEQ,
*ENERGY PRINT, FREQ=1 
 ALLKE,ALLSE,ALLWK,ALLIE,ETOTAL
*NODE PRINT,FREQ=1
 U,
 COORD,
 RF,
*EL FILE, DIRECTIONS=YES
 S,E
*NODE FILE
 U,COORD
*OUTPUT,FIELD,VARIABLE=PRESELECT,FREQUENCY=9999
*OUTPUT,FIELD
*ELEMENT OUTPUT
 S,E
*OUTPUT,HISTORY
*ELEMENT OUTPUT, ELSET=QA_TEST_ALLELEMS
 S,E
*OUTPUT,FIELD
*NODE OUTPUT
 U,COORD
*OUTPUT,HISTORY
*NODE OUTPUT, NSET=QA_TEST_ALLNODES
 U,COORD
*ENERGY OUTPUT
*END STEP